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1993-03-15
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608b
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18 lines
\<COLOUR 1> LAUNCH VEHICLE: \<COLOUR 0> Gemini-Titan
\<COLOUR 1> HEIGHT: \<COLOUR 0> 33 metres
\<COLOUR 1> LIFT-OFF THRUST: \<COLOUR 0> 195 tonnes
\<COLOUR 1> NO OF STAGES: \<COLOUR 0> 2
\<COLOUR 1> PROPELLANTS: \<COLOUR 0> Both stages, Aerozine/nitrogen tetroxide
\<COLOUR 1> PAYLOAD: \<COLOUR 0> Gemini spacecraft
\<COLOUR 1> LAUNCH SITE: \<COLOUR 0> Cape Canaveral, Florida
\<COLOUR 1> COUNTRY: \<COLOUR 0> USA
\<COLOUR 1> COMMENTS: \<COLOUR 0> The launcher used for the 12 Gemini two-man flights in 1965/66; a modified Titan 2 ICBM (intercontinental ballistic missile).